The various engine deterioration phenomena that affect JT9D performance retention were studied, and approaches to improve performance retention of engines were identified. The program included surveys of historical data, monitoring of in service engines, ground and flight testing of instrumented engines, analysis, and analytical modeling. Performance deterioration is made up of both short and long term modes, both of which are flight cycle related phenomena. Short term deterioration occurs primarily during airplane acceptance testing prior to delivery to the airline. This effect is caused by flight load and power induced clearance closures and engine deflections with resulting rubbing of airfoils and seals. Long term deterioration is caused...
Fuel consumption of commercial aircraft is considered. Fuel saving and retention components for new ...
Cruise cockpit recordings and test cell performance data in conjunction with hardware inspection dat...
The JT9D jet engine exhibits a TSFC loss of about 1 percent in the initial 50 flight cycles of a new...
The results of the collection and analysis of historical data pertaining to the deterioration of JT9...
The results of a flight loads test of the JT9D-7 engine are presented. The goals of this test progra...
Results of analyses of engine performance deterioration trends and levels with respect to service us...
An engine was specially prepared with extensive instrumentation to monitor performance, case tempera...
The results of engine performance deterioration investigations based on historical data, special eng...
Cockpit cruise recordings and test cell data in conjunction with hardware inspection results from ai...
Data and engine parts on in-service JT3D and JT8D engines were analyzed and documented relative to e...
An understanding of the mechanisms of deterioration is essential in order that features to counterac...
JT8D and JT9D component performance improvement concepts which have a high probability of incorporat...
A feasibility analysis screening method for predicting the airline acceptance of a proposed engine p...
Flight loads on the 747 propulsion system and resulting JT9D blade to outer airseal running clearanc...
Studies conducted as part of the NASA-Lewis CF6 jet engine diagnostics program are summarized. An 82...
Fuel consumption of commercial aircraft is considered. Fuel saving and retention components for new ...
Cruise cockpit recordings and test cell performance data in conjunction with hardware inspection dat...
The JT9D jet engine exhibits a TSFC loss of about 1 percent in the initial 50 flight cycles of a new...
The results of the collection and analysis of historical data pertaining to the deterioration of JT9...
The results of a flight loads test of the JT9D-7 engine are presented. The goals of this test progra...
Results of analyses of engine performance deterioration trends and levels with respect to service us...
An engine was specially prepared with extensive instrumentation to monitor performance, case tempera...
The results of engine performance deterioration investigations based on historical data, special eng...
Cockpit cruise recordings and test cell data in conjunction with hardware inspection results from ai...
Data and engine parts on in-service JT3D and JT8D engines were analyzed and documented relative to e...
An understanding of the mechanisms of deterioration is essential in order that features to counterac...
JT8D and JT9D component performance improvement concepts which have a high probability of incorporat...
A feasibility analysis screening method for predicting the airline acceptance of a proposed engine p...
Flight loads on the 747 propulsion system and resulting JT9D blade to outer airseal running clearanc...
Studies conducted as part of the NASA-Lewis CF6 jet engine diagnostics program are summarized. An 82...
Fuel consumption of commercial aircraft is considered. Fuel saving and retention components for new ...
Cruise cockpit recordings and test cell performance data in conjunction with hardware inspection dat...
The JT9D jet engine exhibits a TSFC loss of about 1 percent in the initial 50 flight cycles of a new...